KVD-1

KVD-1 was an upper stage LOX/LH₂ cryogenic engine developed by the Isayev Design Bureau (now KB KhIMMASH) of Russia in the early 1960s. It is a modified version of the RD-56, developed for a never-completed cryogenic upper stage of the N-1 super-heavy lift rocket, with the goal of enabling crewed lunar missions by the USSR. The KVD-1 produces a thrust of 7.5 tonnes.

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cryogenic rocket engine, 
cryogenic rocket engine, Dong Fang Hong 2, 

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Frameless

Type	Subtype	Date	Description	Notes	Source